AD 81-15-02

Active

Float Gear Mounting Brackets

Key Information
81-15-02
Active
August 07, 1981
July 13, 1981
Unknown
39-4154
Applicability
["Aircraft"]
["Rotorcraft"]
Airbus Helicopters
AS350B AS350C AS350D AS350D1
Regulatory Text

81-15-02 SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE (SNIAS): Amendment 39-4154. Applies to Models AS350B, AS350C, AS350D, and AS350D-1 helicopters equipped with Air Cruisers' emergency flotation gear Model D24724 in accordance with STC SH2825SW (AS350C, AS350D, AS350D-1) or SH4032SW (AS350B), certificated in all categories (Airworthiness Docket No. 81-ASW-30).

Compliance required as indicated.

To prevent possible failure of the emergency float gear mounting brackets, P/N D16532- 2, D16625-3, and D16625-4, due to fatigue cracks, accomplish the following within the next 10 hours' time in service after the effective date of this AD, unless already accomplished.

a. Conduct a dimensional inspection of the four float mounting brackets, in accordance with Figure 1 of Aerospatiale Helicopter Corp. Service Bulletin No. SB350-13, dated May 22, 1981, to determine which part number brackets are installed.

b. If machined brackets, P/N D16532-1, D16625-1, and D16625-2 are installed, no further action is necessary.

c. If cast brackets, P/N D16532-2, D16625-3, and D16625-4, are installed, remove and replace with machined brackets, P/N D16532-1, D16625-1, and D16625-2.

d. The helicopter may be flown in accordance with FAR 21.197 to a base where the inspection can be performed.

This amendment becomes effective August 7, 1981.

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References
Federal Register Volume 46, Number 133 (Monday, July 13, 1981)
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Issuing Office
["AIR-730: International Validation Branch"]
FAA Documents